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Fiber Optic Gyroscope INS​ (FOG-INS)-Attitude and Heading Reference System (AHRS)
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Fiber Optic Gyroscope INS​ (FOG-INS)-Attitude and Heading Reference System (AHRS)
  • name

Fiber Optic Gyroscope INS​ (FOG-INS)-Attitude and Heading Reference System (AHRS)

MOQ: 1
Price: 155000RMB
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 7days
Payment Method: T/T
Supply Capacity: 100/1day
Details Information
Product Description
Detail Information
Place of Origin
china
Brand Name
CSSC
Certification
TGKM586304752
Model Number
M03MM
Highlight:

Fiber Optic Gyroscope INS

,

FOG-INS AHRS system

,

Fiber Optic Inertial Navigation System

Product Description
Accelerometer Months Bias Repeatability(1σ) ≤50μg
Months Scale Factor Accuracy(1σ) ≤50ppm
Gyro Bias Repeatability(1σ) ≤0.02°/hr
Scale Factor Accuracy(1σ) ≤50ppm
Random walk(1σ) ≤0.006°/√hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration ＞25g
Speed accuracy(Pure inertia) ≤3.0kn,RMS
Speed accuracy(GNSS combination) ≤0.4kn,RMS
Angular Attitude  Any Orientation
Startup time ≤10 sec
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time ≤15min
Position accuracy Pure inertia ≤4nm/1h,CEP
INS/DVL Combination ≤0.6%D,RMS
INS/GNSS Combination better than satellite accuracy
Heading Accuracy Pure inertia ≤0.2°sec(L),RMS
INS/GNSS combination ≤0.1°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.04°,RMS
INS/GNSS combination ≤0.02°,RMS
Characteristics Power consumption ＜15W
Dimensions(Lmm×Wmm×Hmm) 110×110×100
Weight ＜1.7kg
Temperature  -40℃~60℃
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF ＞20000 hours


Tags: 

strapdown inertial system,  

fog inertial navigation system,  

fog ins

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Products
PRODUCTS DETAILS
Products

Laser Inertial Navigation System

Fiber Optic Inertial Navigation System

Aircraft Inertial Navigation System

Marine Inertial Navigation System

Automotive Inertial Navigation System

AHRS System

IMU Inertial Measurement Unit

Fiber Optic Gyroscope

Ring Laser Gyroscope

Doppler Velocity Log
Fiber Optic Gyroscope INS​ (FOG-INS)-Attitude and Heading Reference System (AHRS)
  • name
Fiber Optic Gyroscope INS​ (FOG-INS)-Attitude and Heading Reference System (AHRS)
MOQ: 1
Price: 155000RMB
Standard Packaging: 30cm*30cm*28cm
Delivery Period: 7days
Payment Method: T/T
Supply Capacity: 100/1day
Detail Information
Product Description
Detail Information
Place of Origin
china
Brand Name
CSSC
Certification
TGKM586304752
Model Number
M03MM
Minimum Order Quantity:
1
Price:
155000RMB
Packaging Details:
30cm*30cm*28cm
Delivery Time:
7days
Payment Terms:
T/T
Supply Ability:
100/1day
Highlight

Fiber Optic Gyroscope INS

,

FOG-INS AHRS system

,

Fiber Optic Inertial Navigation System

Product Description
Accelerometer Months Bias Repeatability(1σ) ≤50μg
Months Scale Factor Accuracy(1σ) ≤50ppm
Gyro Bias Repeatability(1σ) ≤0.02°/hr
Scale Factor Accuracy(1σ) ≤50ppm
Random walk(1σ) ≤0.006°/√hr
Features Angular Rate ≥±400°/sec
Angular Acceleration 100000°/sec2
Acceleration ＞25g
Speed accuracy(Pure inertia) ≤3.0kn,RMS
Speed accuracy(GNSS combination) ≤0.4kn,RMS
Angular Attitude  Any Orientation
Startup time ≤10 sec
Input/output 3 RS422 full-duplex serial ports, 1 100M Ethernet port
Alignment time ≤15min
Position accuracy Pure inertia ≤4nm/1h,CEP
INS/DVL Combination ≤0.6%D,RMS
INS/GNSS Combination better than satellite accuracy
Heading Accuracy Pure inertia ≤0.2°sec(L),RMS
INS/GNSS combination ≤0.1°,RMS
Pitch & Roll Accuracy Pure inertia ≤0.04°,RMS
INS/GNSS combination ≤0.02°,RMS
Characteristics Power consumption ＜15W
Dimensions(Lmm×Wmm×Hmm) 110×110×100
Weight ＜1.7kg
Temperature  -40℃~60℃
Shock 15g,Half-sine wave 11ms
Input Voltage DC24V(±25%)
cooling Conduction to mounting plate
Vibration  20~2000Hz,6.06g
MTBF ＞20000 hours


Tags: 

strapdown inertial system,

fog inertial navigation system,

fog ins

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